Wireless and Battery less Accelerometry for Aircraft Structural Health Monitoring

被引:0
作者
Montheard, R. [1 ]
Escriba, C. [1 ]
Fourniols, J. -Y. [1 ]
Lastapis, M. [1 ]
Prunet, J. -M.
Bafleur, M. [1 ,2 ]
Dilhac, J. -M. [1 ,2 ]
机构
[1] CNRS, LAAS, 7 Ave Colonel Roche, F-31077 Toulouse, France
[2] Univ Michigan, Ann Arbor, MI 48109 USA
来源
STRUCTURAL HEALTH MONITORING 2011: CONDITION-BASED MAINTENANCE AND INTELLIGENT STRUCTURES, VOL 1 | 2011年
关键词
D O I
暂无
中图分类号
R5 [内科学];
学科分类号
1002 ; 100201 ;
摘要
This paper presents the design of a self-powered impact sensor dedicated to Structural Health Monitoring for aeronautic applications. The purpose of this work is to identify and implement technological solutions that meet specific requirements for on-ground operation. A prototype featuring thermal energy harvesting, super-capacitor-based energy storage and 3D-accelerometry is demonstrated.
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收藏
页码:471 / +
页数:2
相关论文
共 3 条
[1]  
Lastapis M., 2010, AS PAC WORKSH STRUCT
[2]  
Meekhun D., 2009, 35 ANN C IEEE IND EL
[3]  
Prunet J., 1941, European Patent EP1941475, Patent No. 1941475